WO2001065666A1 - Fail-safe mechanism for dc-drive - Google Patents

Fail-safe mechanism for dc-drive Download PDF

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Publication number
WO2001065666A1
WO2001065666A1 PCT/DE2001/000592 DE0100592W WO0165666A1 WO 2001065666 A1 WO2001065666 A1 WO 2001065666A1 DE 0100592 W DE0100592 W DE 0100592W WO 0165666 A1 WO0165666 A1 WO 0165666A1
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WO
WIPO (PCT)
Prior art keywords
armature winding
winding
drive according
separating means
control unit
Prior art date
Application number
PCT/DE2001/000592
Other languages
German (de)
French (fr)
Inventor
Harald Witzig
Original Assignee
Robert Bosch Gmbh
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from DE10100159A external-priority patent/DE10100159A1/en
Application filed by Robert Bosch Gmbh filed Critical Robert Bosch Gmbh
Priority to EP01913661A priority Critical patent/EP1177609B1/en
Priority to US09/980,691 priority patent/US6759823B2/en
Publication of WO2001065666A1 publication Critical patent/WO2001065666A1/en

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Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K3/00Details of windings
    • H02K3/04Windings characterised by the conductor shape, form or construction, e.g. with bar conductors
    • H02K3/28Layout of windings or of connections between windings
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K11/00Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection
    • H02K11/20Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection for measuring, monitoring, testing, protecting or switching
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K11/00Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection
    • H02K11/20Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection for measuring, monitoring, testing, protecting or switching
    • H02K11/27Devices for sensing current, or actuated thereby
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K11/00Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection
    • H02K11/30Structural association with control circuits or drive circuits
    • H02K11/33Drive circuits, e.g. power electronics
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02HEMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
    • H02H7/00Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions
    • H02H7/08Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for dynamo-electric motors
    • H02H7/0833Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for dynamo-electric motors for electric motors with control arrangements
    • H02H7/0844Fail safe control, e.g. by comparing control signal and controlled current, isolating motor on commutation error
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K29/00Motors or generators having non-mechanical commutating devices, e.g. discharge tubes or semiconductor devices

Definitions

  • the invention is based on a brushless DC drive according to the preamble of patent claim 1.
  • These direct current drives have a synchronous rotor with a stator or armature winding, preferably connected in a star, and a permanently excited rotor.
  • the armature winding is connected to the DC voltage network via a 3-circuit converter with six semiconductor circuit breakers.
  • the inverter which commutates the armature winding, is controlled by an electronic control unit.
  • An example of a synchronous motor operated on a DC voltage network is shown in DE 37 09 168 AI described.
  • Circuit breakers fail, so the DC drive can generate a permanent electromagnetic braking torque without a DC voltage being applied, since the synchronous motor now works as a generator against a low-resistance load resistor.
  • a braking torque affects the function of the unit or system in which the DC drive is used. So z. B. in electric power steering, the braking torque occurring in the event of a fault, considerable steering forces to be exerted by the driver, which cannot be accepted. It is therefore known to provide devices on such DC drives which, in the event of a fault, lead to a so-called fail-silent behavior of the DC drive, ie. That is, the DC drive has no disruptive or adverse influence on the unit or the system, so it works as if the drive was not present.
  • a mechanical clutch is used to generate the desired fail-silent behavior, via which the output shaft of the synchronous motor engages in the steering gear.
  • the brushless DC drive according to the invention with the features of claim 1 has the advantage that the desired fail-silent behavior of the DC drive without expensive external components, such as mechanical clutches, is achieved with simple circuit measures in the drive itself. This makes the DC drive more compact and requires less installation space, so that it can be used in a variety of ways. The additional costs that have to be paid for the desired behavior of the DC drive in the event of a fault are significantly reduced.
  • the separating means for separating the connections between the development phases of the armature winding can be activated by a control unit which recognizes the fault.
  • the control unit has measuring shunts arranged in each connecting line between the switching device designed as a bridge circuit with semiconductor switches and the armature winding.
  • the currents flowing over the measuring shunts are measured in simultaneous blocking phases of all semiconductor switches, and if a current value which differs significantly from zero occurs in one of the measuring shunts, the control device issues an activation signal release agents.
  • Such a design of the control unit, with which errors occurring in the switching device are detected has the advantage that the measuring shunts already present for other reasons for measuring the current in the direct current drive can be used to detect the fault, which further reduces the circuit complexity.
  • Faults in the armature winding itself can e.g. B. detected by measuring the output torque on the output shaft of the synchronous motor, which is advantageous in electric power steering systems, since sensors for measuring the torques occurring on the input and output shafts are already present in the actuators of the electric steering devices.
  • the control unit in the case of a star connection of the armature winding, has measuring shunts which each connect a winding phase of the armature winding to the star point.
  • the control unit continuously measures the currents flowing over the measuring shunts according to magnitude and phase and vectorially adds the shunt currents. If the addition result deviates significantly from zero, the control unit sends an activation signal to the separating means. With such a control unit, errors in the semiconductor switching device as well as errors in the armature winding are recognized and the separating means are activated accordingly.
  • the separating means can be designed in such a way that they irreversibly or reversibly separate the connections between the winding phases of the armature winding.
  • An irreversible separation can be brought about by means of pyrotechnic explosive charges or by means of fuses. Electrical contacts that can be controlled electronically or mechanically are used for the reversible separation.
  • armature windings in a star connection the star point is separated; in the case of armature windings in a delta connection, each winding phase must be disconnected from the winding connections.
  • 1 is a circuit diagram of a brushless DC drive
  • Fig. 2 is a circuit diagram of a modified
  • FIG. 3 shows a circuit diagram of the armature winding of the direct current drive in FIG. 1 with a modified control unit for actuating separating means for separating the armature winding
  • the brushless DC drive shown in the basic circuit diagram in FIG. 1 has a synchronous motor which is operated by means of a switching device 11 for electronic commutation at a DC voltage source 10.
  • the synchronous motor shown here only with its stator or armature winding 12 has in a known manner a stator or stator receiving the armature winding 12 and a rotor or rotor rotating in the stator
  • the three-phase armature winding 12 has three star-connected winding phases 13, the connections 1, 2 and 3 of which are connected to the switching device 11 via a connecting line 14.
  • the switching device 11 designed as a B6 inverter has six semiconductor switches 15, preferably MOS-FETS, which are arranged in a bridge circuit.
  • the connecting lines 14 leading to the winding connections 1, 2 and 3 are each connected to the tap 4, 5 and 6 of a bridge branch, each of which is formed by connecting two semiconductor switches 15 in series and which lies in the connection between the two semiconductor switches 15.
  • the semiconductor switches 15 can be controlled by an electronic control unit 16.
  • the brushless DC drive has one
  • This device for enforcing so-called fail-silent behavior, which ensures that when an error occurs in the DC drive, the z. B. can be caused by a defective semiconductor switch 15 or a winding short in the armature winding 12, the system cooperating with the DC drive is not adversely affected or disturbed.
  • This device comprises separating means which in the event of a fault break the connections between the winding phases 13 and a control unit 17 integrated in the control unit 16 which on the one hand detects the fault and on the other hand activates the separating means when the fault occurs.
  • the control unit 17 includes three measuring shunts, one of which is switched into the three connecting lines 14 between the switching device 11 and the armature winding 12.
  • the control unit 17 measures the shunt currents flowing over the measuring shunts 18 at time intervals in which all the semiconductor switches 15 are blocked. If all semiconductor switches 15 are intact, each shunt current is zero. If the control unit 17 measures a value deviating significantly from zero in one of the measuring shunts 18, it generates an activation signal which is sent to the separating means and activates them.
  • the separating means attack in the star point 20 of the armature winding 12 and, when activated, bring about an irreversible separation of the
  • the separating means are designed here, for example, as a pyrotechnic detonator 19, as used, for. B. is used in motor vehicles to trigger the airbags in the event of a crash.
  • the electrically ignitable detonator 19 is connected on the one hand via a connecting line 40 to the control unit 17 and on the other hand to the negative potential of the DC voltage source 10. If one of the measuring shunts 18 delivers a current value that deviates significantly from zero, the control unit 17 generates an electrical ignition pulse which ignites the detonator capsule 19. The exploding explosive charge tears open the star point 20 and the winding phases 13 are separated from one another. As a result, the system-inherent DC drive, which is driven by the system via its output shaft in the event of a fault, cannot generate any braking torque, since the separated armature winding 12 does not permit generator operation.
  • control unit 17 With the control unit 17 described for FIG. 1, only those errors can be recognized which are based on defects in the semiconductor switches 15. 3, the control unit 17 is modified in such a way that the measuring shunts 18 present in the feed lines 14 are omitted and instead measuring shunts 21 are arranged between the star point 20 and each winding phase 13.
  • the control unit 17 measures the currents flowing through the measuring shunts 21 according to magnitude and phase and adds them vectorially. If the DC motor is fault-free, the addition result always results in zero.
  • the control unit 17 If the vector sum deviates significantly from zero, the control unit 17 in turn generates an activation signal for the separating means which also attack the star point 20.
  • the separating means have a fuse 22, which is briefly heated when activated by the control unit 17 so that it melts through and thus separates the star point 20.
  • a heating coil 24 is used, which is connected to the DC voltage source 10 via a circuit breaker controlled by the control unit 17.
  • the armature winding 12 of the synchronous motor can of course also be connected in a triangle, for example, as shown in the circuit diagram in FIG. 2.
  • the winding phases 13 are connected to the winding connections 1, 2 and 3.
  • the separating means for separating the winding phases 13 in the event of a fault are integrated in the winding phases 13 and connected in series with them. In the exemplary embodiment in FIG. 2, when released, the separating means cause the armature winding 12 to be reversibly separated
  • Winding connections 1, 2 and 3 and the winding phases 13 each have an electrical switching contact 23 which can be controlled electronically or mechanically.
  • Electronically controllable switching contacts 23 are implemented, for example, by transistors or thyristors, mechanically controllable switching contacts 23 can be implemented, for example, as an electromagnetic relay.
  • the separating means are arranged at the star point 20 of the armature winding 12 and, when activated, cause the star point 20 to be irreversibly opened.
  • the separating means had two switching contacts 25 biased in the opening direction, each of a holding member 26 set in the closed position are.
  • a switch contact 25 with a holding element 26 is arranged between the star point 20 and the winding end of two winding phases 13. The provision of a third switching contact with a holding element between star point 20 and the third winding phase 13 is not necessary.
  • the two holding members 26 are assigned a common, electronically ignitable, pyrotechnic detonator 27, which is designed so that it can destroy both holding members 26 when triggered.
  • the detonator 27 is connected via the connecting line 40 to the control unit 17, which in the event of a fault applies an electrical ignition pulse to the detonator 27.
  • the holding members 26 are destroyed, the prestressed switching contacts 25 are released and open them, so that the connection of the two winding phases 13 to the star point 20 is suddenly interrupted.
  • Fig. 4 is a constructive embodiment for the two switch contacts 25 biased in the opening direction with holding member 26 and common detonator 27 for the
  • Holding members 26 shown schematically. Each switch contact 25 has a contact plate 28 which is fixedly connected to an actuating pin 29.
  • the axially displaceable confirmation pin 29 is loaded by a compression spring 30, which is on the one hand with the
  • Actuating pin 29 connected spring plate 31 and supported on a fixed stop 32 and biasing the actuating pin 29 so that the contact plate 28 lifts from the contact points 33, 34.
  • the two cold links 26 have a common locking block 35, in which the two actuating pins 29, each with one on the Engage contact plate 28 pioneering end trained locking lug 36.
  • the detonator 27 is arranged, which in their ⁇ 0 erriegelungblock the ignition destroyed 35th
  • the switching contacts 25 are closed by pressing the contact plate 28 onto the contact points 33, 34 while the compression springs 30 are being tensioned, the locking lug 36 falling into the locking block 35 and being held there.
  • the control unit 17 detonates the detonator 27. This destroys the locking block 35, so that the actuating pins 29 are released and the prestressed compression springs 30 lift the contact plates 28 from the contact points 33, 34.
  • each holding member 26 is assigned to each holding member 26 a separate detonator 27 which, when triggered, destroys the holding member 26, so that the switch contact 25 biased in the closed position opens automatically.
  • a common detonator 27 it is also possible to use a common detonator 27 to destroy all three holding members 26.
  • the prestressed switching contacts 25 with the holding member 26 can be designed as described for FIG. 4.
  • the switching contacts 25 are designed as pretensioned spring tongues
  • the separate compression springs 30 for opening the switching contacts 25 can be dispensed with.

Abstract

The invention relates to a brushless DC-drive, with a synchronous motor, comprising a multi-phase armature winding (12) and a switch device (11), controlled by an electronic controller (16), connected in series with the armature winding (12) for commutating said armature winding (12). According to the invention, separating means (19) are provided to force a fail-safe operation with simple circuitry and without external components in the armature winding (12), said separating means are activated in case of failure and separate the connections between the winding phases (13), preferably at the star point (20).

Description

FAIL- SAFE FÜR BÜRSTENLOSE GLEICHSTROMANTRIEBE .FAIL SAFE FOR BRUSHLESS DC POWER DRIVES.
Stand der TechnikState of the art
Die Erfindung geht aus von einem bürstenlosen Gleichstromantrieb nach dem Oberbegriff des Patentanspruchs 1.The invention is based on a brushless DC drive according to the preamble of patent claim 1.
In Kraftfahrzeugen werden permanenterregte, bürstenloseIn vehicles are permanently excited, brushless
Gleichstromantriebe zu vielfältigen Zwecken, darunter auch für elektrische Servolenkungen, verwendet. Diese Gleichstromantriebe weisen einen Synchronrnotor mit einer vorzugsweise in Stern geschalteten Stator- oder Ankerwicklung und einem permanenterregten Rotor auf. Die Ankerwicklung ist über einen Umrichter in 3rückenschaltung mit sechs Halbleiter- Leistungsschaltern an das Gleichspannungsnetz angeschlossen. Der die Kommutierung der Ankerwicklung bewirkende Wechselrichter wird von einem elektronischen Steuergerät angesteuert. Ein Beispiel für einen an einem Gleichspannungsnetz betriebenen Synchronmotor ist in der DE 37 09 168 AI beschrieben.DC drives used for a variety of purposes, including for electric power steering. These direct current drives have a synchronous rotor with a stator or armature winding, preferably connected in a star, and a permanently excited rotor. The armature winding is connected to the DC voltage network via a 3-circuit converter with six semiconductor circuit breakers. The inverter, which commutates the armature winding, is controlled by an electronic control unit. An example of a synchronous motor operated on a DC voltage network is shown in DE 37 09 168 AI described.
Treten in der Ankerwicklung und/oder in denOccur in the armature winding and / or in the
Leistungsschaltern Fehler auf, so kann der Gleichstromantrieb ein dauerhaftes elektromagnetisches Bremsmoment erzeugen, ohne daß eine Gleichspannung angelegt ist, da nunmehr der Synchronmotor als Generator gegen einen niederohmigen Lastwiderstand arbeitet. In vielen Anwendungsfällen beeinträchtigt ein solches Bremsmoment die Funktion des Aggregats oder Systems, in dem der Gleichstromantrieb eingesetzt ist. So erzwingt z. B. bei elektrischen Servolenkungen das im Fehlerfall auftretende Bremsmoment erhebliche, vom Fahrer aufzubringende Lenkkräfte, die nicht akzeptiert werden können. Es ist daher bekannt, an solchen Gleichstromantrieben Einrichtungen vorzusehen, die im Fehlerfall zu einem sog. Fail-Silent-Verhalten des Gleichstromantriebs führen, d. h., daß der Gleichstromantrieb keinen störenden oder nachteiligen Einfluß auf das Aggregat oder des System ausübt, dieses also so arbeitet, als ob der Antrieb nicht vorhanden wäre.Circuit breakers fail, so the DC drive can generate a permanent electromagnetic braking torque without a DC voltage being applied, since the synchronous motor now works as a generator against a low-resistance load resistor. In many applications, such a braking torque affects the function of the unit or system in which the DC drive is used. So z. B. in electric power steering, the braking torque occurring in the event of a fault, considerable steering forces to be exerted by the driver, which cannot be accepted. It is therefore known to provide devices on such DC drives which, in the event of a fault, lead to a so-called fail-silent behavior of the DC drive, ie. That is, the DC drive has no disruptive or adverse influence on the unit or the system, so it works as if the drive was not present.
Bei einer bekannten elektrischen Servolenkung wird zur Erzeugung des angestrebten Fail-Silent-Verhaltens eine mechanische Kupplung verwendet, über die die Abtriebswelle des Synchronmotors in das Lenkgetriebe eingreift. ImIn a known electric power steering, a mechanical clutch is used to generate the desired fail-silent behavior, via which the output shaft of the synchronous motor engages in the steering gear. in the
Fehlerfall wird die Kupplung geöffnet und somit der Motor vom Lenksystem abgekoppelt. Vorteile der ErfindungIn the event of a fault, the clutch is opened and the motor is thus disconnected from the steering system. Advantages of the invention
Der erfindungsgemäße bürstenlose Gleichstromantrieb mit den Merkmalen des Patentanspruchs 1 hat den Vorteil, daß das gewünschte Fail-Silent-Verhalten des Gleichstromantriebs ohne teure externe Bauelemente, wie sie mechanische Kupplungen darstellen, mit einfachen Schaltungsmaßnahmen im Antrieb selbst erreicht wird. Damit wird der Gleichstromantrieb kompakter und benötigt weniger Bauraum, so daß er vielseitiger einsetzbar ist. Die Zusatzkosten, die für das erwünschte Verhalten des Gleichstromantriebs im Fehlerfall aufzubringen sind, sind deutlich reduziert.The brushless DC drive according to the invention with the features of claim 1 has the advantage that the desired fail-silent behavior of the DC drive without expensive external components, such as mechanical clutches, is achieved with simple circuit measures in the drive itself. This makes the DC drive more compact and requires less installation space, so that it can be used in a variety of ways. The additional costs that have to be paid for the desired behavior of the DC drive in the event of a fault are significantly reduced.
Durch die in den weiteren Ansprüchen aufgeführten Maßnahmen sind vorteilhafte Weiterbildungen und Verbesserungen des im Patentanspruchs 1 angegebenen Gleichstromantriebs möglich.Advantageous further developments and improvements of the direct current drive specified in claim 1 are possible through the measures listed in the further claims.
Gemäß einer bevorzugten Ausführungsform der Erfindung sind die Trennmittel zum Auftrennen der Verbindungen zwischen den Wic-klungsphasen der Ankerwicklung durch eine Steuereinheit, die den Fehlerfall erkennt, aktivierbar.According to a preferred embodiment of the invention, the separating means for separating the connections between the development phases of the armature winding can be activated by a control unit which recognizes the fault.
Gemäß einer vorteilhaften Ausführungsform der Erfindung weist hierzu die Steuereinheit in jeder Verbindungsleitung zwischen der als Brückenschaltung mit Halbleiterschaltern ausgebildeten Schaltvorrichtung und der Ankerwicklung angeordnete Meßshunts auf. In gleichzeitigen Sperrphasen aller Halbleiterschalter werden die über die Meßshunts fließenden Ströme gemessen, und bei Auftreten eines signifikant von Null abweichenden Stromwerts in einem der Meßshunts gibt die Steuervorrichtung ein Aktivierungssignal an die Trennmittel aus. Eine solche Ausbildung der Steuereinheit, mit der in der Schaltvorrichtung auftretende Fehler erkannt werden, hat den Vorteil, daß die bereits aus anderen Gründen zur Strommessung in dem Gleichstromantrieb vorhandenen Meßshunts zur Erkennung des Fehlerfalls herangezogen werden können, wodurch sich der Schaltungsaufwand weiter reduziert. Fehler in der Ankerwicklung selbst können z. B. durch Messen des an der Abtriebswelle des Synchronmotors abgegebenen Bremsmoments erfaßt werden, was bei elektrischen Servolenkungen von Vorteil ist, da in den Stellgliedern der elektrischen Lenkvorrichtungen bereits Sensoren zur Messung der an den Eingangs- und Ausgangswellen auftretenden Drehmomente vorhanden sind.According to an advantageous embodiment of the invention, for this purpose the control unit has measuring shunts arranged in each connecting line between the switching device designed as a bridge circuit with semiconductor switches and the armature winding. The currents flowing over the measuring shunts are measured in simultaneous blocking phases of all semiconductor switches, and if a current value which differs significantly from zero occurs in one of the measuring shunts, the control device issues an activation signal release agents. Such a design of the control unit, with which errors occurring in the switching device are detected, has the advantage that the measuring shunts already present for other reasons for measuring the current in the direct current drive can be used to detect the fault, which further reduces the circuit complexity. Faults in the armature winding itself can e.g. B. detected by measuring the output torque on the output shaft of the synchronous motor, which is advantageous in electric power steering systems, since sensors for measuring the torques occurring on the input and output shafts are already present in the actuators of the electric steering devices.
Gemäß einer vorteilhaften Ausführungsform der Erfindung weist bei einer Sternschaltung der Ankerwicklung die Steuereinheit Meßshunts auf, die jeweils eine Wicklungsphase der Ankerwicklung mit dem Sternpunkt verbinden. Die Steuereinheit mißt fortlaufend die über die Meßshunts fließenden Ströme nach Betrag und Phase und addiert die Shuntströ e vektoriell. Bei einem signifikanten Abweichen des Additionsergebnisses von Null gibt die Steuereinheit ein Aktivierungssignal an die Trennmittel. Mit einer solchen Steuereinheit werden sowohl Fehler in der Halbleiter-Schaltvorrichtung als auch Fehler in der Ankerwicklung erkannt und entsprechend die Trennmittel aktiviert .According to an advantageous embodiment of the invention, in the case of a star connection of the armature winding, the control unit has measuring shunts which each connect a winding phase of the armature winding to the star point. The control unit continuously measures the currents flowing over the measuring shunts according to magnitude and phase and vectorially adds the shunt currents. If the addition result deviates significantly from zero, the control unit sends an activation signal to the separating means. With such a control unit, errors in the semiconductor switching device as well as errors in the armature winding are recognized and the separating means are activated accordingly.
Gemäß vorteilhafter Ausführungsformen der Erfindung können die Trennmittel so ausgebildet sein, daß sie eine irreversible oder reversible Auftrennung der Verbindungen zwischen den Wicklungsphasen der Ankerwicklung bewirken. Eine irreversible Auftrennung kann mittels pyrotechnischer Sprengladungen oder mittels Schmelzsicherungen herbeigeführt werden. Für die reversible Auftrennung werden elektrische Kontakte verwendet, die elektronisch oder mechanisch steuerbar sind. Bei Ankerwicklungen in Sternschaltung wird der Sternpunkt aufgetrennt, bei Ankerwicklungen in Dreieckschaltung muß jede Wicklungsphase von den Wicklungsanschlüssen abgetrennt werden.According to advantageous embodiments of the invention, the separating means can be designed in such a way that they irreversibly or reversibly separate the connections between the winding phases of the armature winding. An irreversible separation can be brought about by means of pyrotechnic explosive charges or by means of fuses. Electrical contacts that can be controlled electronically or mechanically are used for the reversible separation. In the case of armature windings in a star connection, the star point is separated; in the case of armature windings in a delta connection, each winding phase must be disconnected from the winding connections.
Zeichnungdrawing
Die Erfindung ist anhand von in der Zeichnung dargestellten Ausführungsbeispielen in der nachfolgenden Beschreibung näher erläutert. Es zeigen:The invention is explained in more detail in the following description with reference to exemplary embodiments shown in the drawing. Show it:
Fig. 1 ein Schaltbild eines bürstenlosen Gleichstromantriebs,1 is a circuit diagram of a brushless DC drive,
Fig. 2 ein Schaltbild einer modifiziertenFig. 2 is a circuit diagram of a modified
Ankerwicklung für den Gleichstromantrieb in Figur 1,Armature winding for the direct current drive in FIG. 1,
Fig. 3 ein Schaltbild der Ankerwicklung des Gleichstromantriebs in Fig. 1 mit modifizierter Steuereinheit zum Ansteuern von Trennmitteln zum Auftrennen der Ankerwicklung,3 shows a circuit diagram of the armature winding of the direct current drive in FIG. 1 with a modified control unit for actuating separating means for separating the armature winding,
Fig. 4 jeweils eine gleiche Darstellung wie in Fig. 2 und 5 gemäß zweier weiterer Ausführungsbeispiele. Beschreibung der Ausführungsbeispiele4 each show the same representation as in FIGS. 2 and 5 according to two further exemplary embodiments. Description of the embodiments
Der in Fig. 1 im Prinzipschaltbild dargestellte bürstenlose Gleichstromantrieb weist einen Synchronmotor auf, der mittels einer Schaltvorrichtung 11 zum elektronischen Kommutieren an einer Gleichspannungsquelle 10 betrieben wird. Der hier nur mit seiner Stator- oder Ankerwicklung 12 dargestellte Synchronmotor weist in bekannter Weise einen die Ankerwicklung 12 aufnehmenden Stator oder Ständer und einen im Stator drehenden Rotor oder Läufer mitThe brushless DC drive shown in the basic circuit diagram in FIG. 1 has a synchronous motor which is operated by means of a switching device 11 for electronic commutation at a DC voltage source 10. The synchronous motor shown here only with its stator or armature winding 12 has in a known manner a stator or stator receiving the armature winding 12 and a rotor or rotor rotating in the stator
Permanentmagnetpolen auf. Die dreiphasig ausgeführte Ankerwicklung 12 weist im Ausführungsbeispiel der Fig. 1 drei in Stern geschaltete Wicklungsphasen 13 auf, deren Anschlüsse 1, 2 und 3 über Verbindungsleitung 14 mit der Schaltvorrichtung 11 verbunden sind.Permanent magnet poles. In the exemplary embodiment in FIG. 1, the three-phase armature winding 12 has three star-connected winding phases 13, the connections 1, 2 and 3 of which are connected to the switching device 11 via a connecting line 14.
Die als B6-Wechselrichter ausgeführte Schaltvorrichtung 11 weist sechs Halbleiterschalter 15, vorzugsweise MOS-FETS, auf, die in Brückenschaltung angeordnet sind. Die zu den Wicklungsanschlüssen 1,2 und 3 führenden Verbindungsleitungen 14 sind dabei jeweils an dem Abgriff 4, 5 und 6 eines jeweils durch Reihenschaltung zweier Halbleiterschalter 15 gebildeten Brückenzweigs angeschlossen, der in der Verbindung der beiden Halbleiterschalter 15 liegt. Zum Kommutieren der Ankerwicklung 12, d. h. zum zeitlich richtigen Anlegen der Wicklungsphasen 13 an die Gleichspannungsquelle 10, sind die Halbleiterschalter 15 von einem elektronischen Steuergerät 16 ansteuerbar.The switching device 11 designed as a B6 inverter has six semiconductor switches 15, preferably MOS-FETS, which are arranged in a bridge circuit. The connecting lines 14 leading to the winding connections 1, 2 and 3 are each connected to the tap 4, 5 and 6 of a bridge branch, each of which is formed by connecting two semiconductor switches 15 in series and which lies in the connection between the two semiconductor switches 15. To commutate the armature winding 12, d. H. For the correct application of the winding phases 13 to the DC voltage source 10, the semiconductor switches 15 can be controlled by an electronic control unit 16.
Der bürstenlose Gleichstromantrieb verfügt über eineThe brushless DC drive has one
Einrichtung zum Erzwingen eines sog. Fail-Silent-Verhaltens, die sicherstellt, daß bei Auftreten eines Fehlers im Gleichstromantrieb, der z. B. von einem defekten Halbleiterschalter 15 oder einem Wicklungsschluß in der Ankerwicklung 12 verursacht sein kann, das mit dem Gleichstromantrieb zusammenwirkende System nicht nachteilig beeinflußt oder gestört wird. Diese Einrichtung umfaßt Trennmittel, die im Fehlerfall die Verbindungen zwischen den Wicklungsphasen 13 auftrennen sowie eine im Steuergerät 16 integrierte Steuereinheit 17, die einerseits den Fehlerfall erfaßt und andererseits die Trennmittel bei Auftreten des Fehlerfalls aktiviert. Im Ausführungsbeispiel der Fig. 1 gehören zu der Steuereinheit 17 drei Meßshunts, von denen jeweils einer in die drei Verbindungsleitungen 14 zwischen Schaltvorrichtung 11 und Ankerwicklung 12 eingeschaltet ist.Device for enforcing so-called fail-silent behavior, which ensures that when an error occurs in the DC drive, the z. B. can be caused by a defective semiconductor switch 15 or a winding short in the armature winding 12, the system cooperating with the DC drive is not adversely affected or disturbed. This device comprises separating means which in the event of a fault break the connections between the winding phases 13 and a control unit 17 integrated in the control unit 16 which on the one hand detects the fault and on the other hand activates the separating means when the fault occurs. In the exemplary embodiment in FIG. 1, the control unit 17 includes three measuring shunts, one of which is switched into the three connecting lines 14 between the switching device 11 and the armature winding 12.
In Zeitintervallen, in denen alle Hälbleiterschalter 15 gesperrt sind, mißt die Steuereinheit 17 die über die Meßshunts 18 fließenden Shuntströme. Sind alle Halbleiterschalter 15 intakt, so ist jeder Shuntstrom Null. Mißt die Steuereinheit 17 in einem der Meßshunts 18 einen signifikant von Null abweichenden Wert, so erzeugt sie ein Aktivierungssignal, das an die Trennmittel gegeben wird und diese aktiviert.The control unit 17 measures the shunt currents flowing over the measuring shunts 18 at time intervals in which all the semiconductor switches 15 are blocked. If all semiconductor switches 15 are intact, each shunt current is zero. If the control unit 17 measures a value deviating significantly from zero in one of the measuring shunts 18, it generates an activation signal which is sent to the separating means and activates them.
Im Ausführungsbeispiel der Fig. 1 greifen die Trennmittel im Sternpunkt 20 der Ankerwicklung 12 an und bewirken bei ihrem Aktivieren ein irreversibles Auftrennen derIn the exemplary embodiment in FIG. 1, the separating means attack in the star point 20 of the armature winding 12 and, when activated, bring about an irreversible separation of the
Sternpunktverbindung der Wicklungsphasen 13. Die Trennmittel sind hier beispielsweise als eine pyrotechnische Sprengkapsel 19 ausgebildet, wie sie z. B. bei Kraftfahrzeugen zur Auslösung der Airbags im Crashfall verwendet wird. Die elektrisch zündbare Sprengkapsel 19 ist einerseits über eine Verbindungsleitung 40 mit der Steuereinheit 17 und andererseits mit dem Minuspotential der Geichspannungsquelle 10 verbunden. Liefert einer der Meßshunts 18 einen signifikant von Null aoweichenden Stromwert, so erzeugt αie Steuereinheit 17 einen elektrischen Zündimpuls, der die Sprengkapsel 19 zündet. Die explodierende Sprengladung reißt den Sternpunkt 20 auf und die Wicklungsphasen 13 sind voneinander getrennt. Dadurch kann der systemimmanente Gleichstromantrieb, der von dem System im Fehlerfall über seine Abtriebswelle angetrieben wird, kein Bremsmoment erzeugen, da die aufgetrennte Ankerwicklung 12 keinen Generatorbetrieb zuläßt.Star point connection of the winding phases 13. The separating means are designed here, for example, as a pyrotechnic detonator 19, as used, for. B. is used in motor vehicles to trigger the airbags in the event of a crash. The electrically ignitable detonator 19 is connected on the one hand via a connecting line 40 to the control unit 17 and on the other hand to the negative potential of the DC voltage source 10. If one of the measuring shunts 18 delivers a current value that deviates significantly from zero, the control unit 17 generates an electrical ignition pulse which ignites the detonator capsule 19. The exploding explosive charge tears open the star point 20 and the winding phases 13 are separated from one another. As a result, the system-inherent DC drive, which is driven by the system via its output shaft in the event of a fault, cannot generate any braking torque, since the separated armature winding 12 does not permit generator operation.
Mit der zu Fig. 1 beschriebenen Steuereinheit 17 können nur solche Fehler erkannt werden, die auf Defekte in den Halbleiterschaltern 15 beruhen. Um auch in der Ankerwicklung 12 auftretende Fehlerrr.öglichkeiten zu erfassen, ist gemäß Fig. 3 die Steuereinheit 17 dahingehend modifiziert, daß die in den Zuleitungen 14 vorhandenen Meßshunts 18 entfallen und statt dessen Meßshunts 21 zwischen dem Sternpunkt 20 und jeder Wicklungsphase 13 angeordnet sind. Die Steuereinheit 17 mißt die über die Meßshunts 21 fließenden Ströme nach Betrag und Phase und addiert diese vektoriell. Bei fehlerfreiem Gleichstrommotor ergibt das Additionsergebnis stets Null.With the control unit 17 described for FIG. 1, only those errors can be recognized which are based on defects in the semiconductor switches 15. 3, the control unit 17 is modified in such a way that the measuring shunts 18 present in the feed lines 14 are omitted and instead measuring shunts 21 are arranged between the star point 20 and each winding phase 13. The control unit 17 measures the currents flowing through the measuring shunts 21 according to magnitude and phase and adds them vectorially. If the DC motor is fault-free, the addition result always results in zero.
Weicht die Vektorsumme signifikant von Null ab, erzeugt die Steuereinheit 17 wiederum ein Aktivierungssignal für die nier ebenfalls am Sternpun.t 20 angreifenden Trennmittel. Im Ausführungsbeispiel der Fig. 3 weisen die Trennmittel eine Schmelzsicherung 22 auf, die bei Aktivierung durch die Steuereinheit 17 kurzfristig so erhitzt wird, daß sie durchschmilzt und damit den Sternpunkt 20 auftrennt. Zur Aufheizung der Schmelzsicherung 22 wird eine Heizwendel 24 verwendet, die über einen von der Steuereinheit 17 gesteuerten Leistungsschalter an der Gleichspannungsquelle 10 angeschlossen ist.If the vector sum deviates significantly from zero, the control unit 17 in turn generates an activation signal for the separating means which also attack the star point 20. In the embodiment of FIG. 3, the separating means have a fuse 22, which is briefly heated when activated by the control unit 17 so that it melts through and thus separates the star point 20. To heat the fuse 22, a heating coil 24 is used, which is connected to the DC voltage source 10 via a circuit breaker controlled by the control unit 17.
Die Ankerwicklung 12 des Synchronmotors kann selbstverständlich auch beispielsweise in Dreieck geschaltet sein, wie dies in Fig. 2 im Schaltbild dargestellt ist. Die Wicklungsphasen 13 sind dabei mit den Wicklungsanschlüssen 1, 2 und 3 verbunden. Die Trennmittel zum Auftrennen der Wicklungsphasen 13 im Fehlerfall sind in αen Wicklungsphasen 13 integriert und mit diesen in Reihe geschaltet. Im Ausführungsbeispiel der Fig. 2 bewirken die Trennmittel bei ihrem Ansprechen eine reversible Auftrennung der Ankerwicklung 12. Hierzu ist zwischen denThe armature winding 12 of the synchronous motor can of course also be connected in a triangle, for example, as shown in the circuit diagram in FIG. 2. The winding phases 13 are connected to the winding connections 1, 2 and 3. The separating means for separating the winding phases 13 in the event of a fault are integrated in the winding phases 13 and connected in series with them. In the exemplary embodiment in FIG. 2, when released, the separating means cause the armature winding 12 to be reversibly separated
Wicklungsanschlüssen 1, 2 und 3 und den Wicklungsphasen 13 jeweils ein elektrischer Schaltkontakt 23 angeordnet, der elektronisch oder mechanisch steuerbar ist. Elektronisch steuerbare Schaltkontakte 23 werden beispielsweise durch Transistoren oder Thyristoren realisiert, mechanisch steuerbare Schaltkontakte 23 können beispielsweise als elektromagnetiscr.es Relais ausgeführt werden.Winding connections 1, 2 and 3 and the winding phases 13 each have an electrical switching contact 23 which can be controlled electronically or mechanically. Electronically controllable switching contacts 23 are implemented, for example, by transistors or thyristors, mechanically controllable switching contacts 23 can be implemented, for example, as an electromagnetic relay.
Im Ausführungsbeispiel der Fig. 4 sind wie bei dem Ausführungsbeispiel gemäß Fig. 1 die Trennmittel am Sternpunkt 20 der Ankerwicklung 12 angeordnet und bewirken bei ihrem Aktivieren ein irreversibles Auftrennen des Sternpunktes 20. Die Trennmittel wiesen zwei in Öffnungsrichtung vorgespannte Schaltkontakte 25 auf, die jeweils von einem Halteglied 26 in Schließstellung festgelegt sind. Jeweils ein Schaltkontakt 25 mit Halteglied 26 ist zwischen dem Sternpunkt 20 und dem Wicklungsende zweier Wicklungsphasen 13 angeordnet. Das Vorsehen eines dritten Schaltkontaktes mit Halteglied zwischen Sternpunkt 20 und der dritten Wicklungsphase 13 ist nicht erforderlich. Den beiden Haltegliedern 26 ist eine gemeinsame, elektronisch zündbare, pyrotechnische Sprengkapsel 27 zugeordnet, die so ausgelegt ist, daß sie bei Auslösung beide Halteglieder 26 zu zerstören vermag. Wie beim Ausführungsbeispiel der Fig. 1 ist die Sprengkapsel 27 über die Verbindungsleitung 40 mit der Steuereinheit 17 verbunden, die im Fehlerfall einen elektrischen Zündimpuls an die Sprengkapsel 27 legt. Mit Zerstörung der Halteglieder 26 werden die vorgespannten Schaltkontakte 25 freigegeben, und diese öffnen, so daß die Verbindung der beiden Wicklungsphasen 13 zum Sternpunkt 20 schlagartig unterbrochen wird.In the exemplary embodiment in FIG. 4, as in the exemplary embodiment in accordance with FIG. 1, the separating means are arranged at the star point 20 of the armature winding 12 and, when activated, cause the star point 20 to be irreversibly opened. The separating means had two switching contacts 25 biased in the opening direction, each of a holding member 26 set in the closed position are. A switch contact 25 with a holding element 26 is arranged between the star point 20 and the winding end of two winding phases 13. The provision of a third switching contact with a holding element between star point 20 and the third winding phase 13 is not necessary. The two holding members 26 are assigned a common, electronically ignitable, pyrotechnic detonator 27, which is designed so that it can destroy both holding members 26 when triggered. As in the exemplary embodiment in FIG. 1, the detonator 27 is connected via the connecting line 40 to the control unit 17, which in the event of a fault applies an electrical ignition pulse to the detonator 27. When the holding members 26 are destroyed, the prestressed switching contacts 25 are released and open them, so that the connection of the two winding phases 13 to the star point 20 is suddenly interrupted.
In Fig. 4 ist ein konstruktives Ausführungsbeispiel für die beiden in Öffnungsrichtung vorgespannten Schaltkontakte 25 mit Halteglied 26 und gemeinsamer Sprengkapsel 27 für dieIn Fig. 4 is a constructive embodiment for the two switch contacts 25 biased in the opening direction with holding member 26 and common detonator 27 for the
Halteglieder 26 schematisch dargestellt. Jeder Schaltkontakt 25 besitzt eine Kontaktplatte 28, die mit einem Betätigungsstift 29 fest verbunden ist. Der axial verschiebbare Bestätigungsstift 29 wird von einer Druckfeder 30 belastet, die sich einerseits an einem mit demHolding members 26 shown schematically. Each switch contact 25 has a contact plate 28 which is fixedly connected to an actuating pin 29. The axially displaceable confirmation pin 29 is loaded by a compression spring 30, which is on the one hand with the
Betätigungsstift 29 verbundenen Federteller 31 und an einem raumfesten Anschlag 32 abstützt und den Betätigungsstift 29 so vorspannt, daß die Kontaktplatte 28 von den Kontaktpunkten 33, 34 abhebt. Die beiden Kalteglieder 26 weisen einen gemeinsamen Verriegelungsblock 35 auf, in denen die beiden Betätigungsstifte 29 mit jeweils einer an ihrem von der Kontaktplatte 28 wegweisenden Ende ausgebildeten Verriegelungsnase 36 eingreifen. Innerhalb des Verriegelungsblocks 35 ist die Sprengkapsel 27 angeordnet, die bei ihrer Zündung den 0τerriegelungblock 35 zerstört. Bei der Montage werden die Schaltkontakte 25 geschlossen, indem die Kontaktplatte 28 unter Spannen der Druckfedern 30 auf die Kontaktpunkte 33, 34 aufgedrückt wird, wobei die Verriegelungsnase 36 in den Verriegelungsblock 35 einfallen und dort gehalten sind. Im Fehlerfall wird von der Steuereinheit 17 die Sprengkapsel 27 gezündet. Diese zerstört den Verriegelungsblock 35, so daß die Betätigungsstifte 29 freigegeben werden und die vorgespannten Druckfedern 30 die Kontaktplatten 28 von den Kontaktpunkten 33, 34 abheben.Actuating pin 29 connected spring plate 31 and supported on a fixed stop 32 and biasing the actuating pin 29 so that the contact plate 28 lifts from the contact points 33, 34. The two cold links 26 have a common locking block 35, in which the two actuating pins 29, each with one on the Engage contact plate 28 pioneering end trained locking lug 36. Within the lock block 35, the detonator 27 is arranged, which in their τ 0 erriegelungblock the ignition destroyed 35th During assembly, the switching contacts 25 are closed by pressing the contact plate 28 onto the contact points 33, 34 while the compression springs 30 are being tensioned, the locking lug 36 falling into the locking block 35 and being held there. In the event of a fault, the control unit 17 detonates the detonator 27. This destroys the locking block 35, so that the actuating pins 29 are released and the prestressed compression springs 30 lift the contact plates 28 from the contact points 33, 34.
Bei dem Ausführungsbeispiel gemäß Fig. 5 ist wie bei dem Ausführungsbeispiel gemäß Fig. 2 die Ankerwicklung 12 in Dreieck geschaltet. Hier ist es erforderlich, daß im Fehlerfall jeder Zweig der Dreieckschaltung aufgetrennt wird, so daß ein Schaltkontakt 25 mit Halteglied 26 mit jeder Wicklungsphase 13 in Reihe geschaltet ist. ImIn the exemplary embodiment according to FIG. 5, as in the exemplary embodiment according to FIG. 2, the armature winding 12 is connected in a triangle. Here it is necessary that, in the event of a fault, each branch of the delta connection is disconnected, so that a switching contact 25 with holding element 26 is connected in series with each winding phase 13. in the
Ausführungsbeispiel der Fig. 5 ist jedem Halteglied 26 eine separate Sprengkapsel 27 zugeordnet, die bei ihrem Auslösen das Halteglied 26 zerstört, so daß der in Schließstellung vorgespannte Schaltkontakt 25 selbsttätig öffnet. Selbstverständlich ist es auch möglich, zur Zerstörung aller drei Halteglieder 26 eine gemeinsame Sprengkapsel 27 zu verwenden. Die vorgespannten Schaltkontakte 25 mit Halteglied 26 können wie zu Fig. 4 beschrieben ausgeführt werden. Bei Ausbildung der Schaltkontakte 25 als vorgespannte Federzungen kann auf die separaten Druckfedern 30 zum Öffnen der Schaltkontakte 25 verzichtet werden. 5 is assigned to each holding member 26 a separate detonator 27 which, when triggered, destroys the holding member 26, so that the switch contact 25 biased in the closed position opens automatically. Of course, it is also possible to use a common detonator 27 to destroy all three holding members 26. The prestressed switching contacts 25 with the holding member 26 can be designed as described for FIG. 4. When the switching contacts 25 are designed as pretensioned spring tongues, the separate compression springs 30 for opening the switching contacts 25 can be dispensed with.

Claims

Patentansprüche claims
1. Bürstenloser Gleichstromantrieb mit einem eine mehrphasige Ankerwicklung (12) 'aufweisenden Synchronmotor, mit einer der Ankerwicklung (12) vorgeschalteten, von einem elektronischen Steuergerät (16) gesteuerten Schaltvorrichtung (11) zum Kommutieren der Ankerwicklung (12) und mit einer Einrichtung zum Erzeugen eines Fail-Silent-Verhaltens, dadurch gekennzeichnet, daß die Einrichtung im Fehlerfall ansprechende Trennmittel aufweist, die die Verbindungen zwischen den Wicklungsphasen (13) der Ankerwicklung (12; auftrennen.1. Brushless DC drive with a multi-phase armature winding (12) ' having a synchronous motor, with an upstream of the armature winding (12), controlled by an electronic control unit (16) switching device (11) for commutating the armature winding (12) and with a device for generating Fail-silent behavior, characterized in that in the event of a fault, the device has appealing separating means which separate the connections between the winding phases (13) of the armature winding (12;
2. Gleichstromantrieb nach Anspruch 1, dadurch gekennzeichnet, daß die Trennmittel durch eine den2. DC drive according to claim 1, characterized in that the separating means by a
Fehlerfall erkennende Steuereinheit (17) aktivierbar sind. Control unit (17) that detects a fault can be activated.
3. Gleichstromantrieb nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß die Trennmittel so ausgebildet sind, daß sie eine irreversible Auftrennung bewirken.3. DC drive according to claim 1 or 2, characterized in that the separating means are designed so that they cause an irreversible separation.
4. Gleichstromantrieb nach Anspruch 3, dadurch gekennzeichnet, daß die Trennmittel mindestens eine von der Steuereinheit (17) auslösbare pyrotechnische Sprengkapsel (19) aufweisen.4. DC drive according to claim 3, characterized in that the separating means have at least one pyrotechnic detonator (19) which can be triggered by the control unit (17).
5. Gleichstromantrieb nach Anspruch 4, dadurch gekennzeichnet, daß die. Ankerwicklung (12) in Stern geschaltet ist und die pyrotechnische Sprengkapsel (19) am Sternpunkt (20) so angeordnet ist, daß sie den Sternpunkt (20) aufzureißen vermag.5. DC drive according to claim 4, characterized in that the. Armature winding (12) is connected in star and the pyrotechnic detonator (19) is arranged at the star point (20) so that it can tear open the star point (20).
6. Gleichstromantrieb nach Anspruch 4, dadurch gekennzeichnet, daß die Trennmittel in Öffnungsrichtung vorgespannte Schaltkontakte (25) und jeweils einen der Schaltkontakte (25) in deren Schließstellung festlegende Halteglieder (26) aufweisen und daß die mindestens eine Sprengkapsel (27) so angeordnet ist, daß sie die Halteglieder (26) zu zerstören oder lösen vermag.6. DC drive according to claim 4, characterized in that the separating means biased switch contacts (25) in the opening direction and each have one of the switch contacts (25) in their closed position fixing holding members (26) and that the at least one detonator (27) is arranged so that it can destroy or detach the holding members (26).
7. Gleichstromantrieb nach Anspruch 6, dadurch gekennzeichnet, daß die Ankerwicklung (12) in Stern geschaltet und zwischen dem Sternpunkt (20) und dem Wicklungsende von mindestens zwei Wicklungsphasen (13) jeweils ein Schaltkontakt (25) mit Halteglied (26) angeordnet ist und daß den beiden Haltegliedern (26) eine gemeinsame Sprengkapsel (27) zugeordnet ist. 7. DC drive according to claim 6, characterized in that the armature winding (12) connected in star and between the star point (20) and the winding end of at least two winding phases (13) each have a switching contact (25) with holding member (26) and that the two holding members (26) are assigned a common detonator (27).
8. Gleichstromantrieb nach Anspruch 6, dadurch gekennzeichnet, daß die Ankerwicklung (12) in Dreieck geschaltet ist und ein Schaltkontakt (25) mit Halteglied (26) mit jeder Wicklungsphase (13) in Reihe geschaltet ist und daß jedem Halteglied (26) eine pyrotechnische Sprengkapsel (27) oder allen Haltegliedern (26) eine gemeinsame Sprengkapsel (27) zugeordnet ist.8. DC drive according to claim 6, characterized in that the armature winding (12) is connected in a triangle and a switching contact (25) with holding member (26) with each winding phase (13) is connected in series and that each holding member (26) has a pyrotechnic Detonator (27) or all holding members (26) are assigned a common detonator (27).
9. Gleichstromantrieb nach Anspruch 3, dadurch gekennzeichnet, daß die Trennmittel mindestens eine von der Steuereinheit (17) ansteuerbare Schmelzsicherung (22) aufweisen.9. DC drive according to claim 3, characterized in that the separating means have at least one of the control unit (17) controllable fuse (22).
10. Gleichstromantrieb nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß die Trennmittel so ausgebildet sind, daß sie eine reversible Auftrennung bewirken.10. DC drive according to claim 1 or 2, characterized in that the separating means are designed so that they bring about a reversible separation.
11. Gleichstromantrieb nach Anspruch 10, dadurch gekennzeichnet, daß die Trennmittel in den Wicklungsphasen (13) angeordnete elektrische11. DC drive according to claim 10, characterized in that the separating means in the winding phases (13) arranged electrical
Schaltkontakte (23) aufweisen, die elektronisch oder mechanisch steuerbar sind.Have switching contacts (23) which can be controlled electronically or mechanically.
12. Gleichstromantrieb nach einem der Ansprüche 9 - 11, dadurch gekennzeichnet, daß die Ankerwicklung (12) in12. DC drive according to one of claims 9 - 11, characterized in that the armature winding (12) in
Stern geschaltet ist und die Trennmittel im Sternpunkt (20) angeordnet sind.Star is switched and the release agent are arranged in the star point (20).
13. Gleichstromantrieb nach einem der Ansprüche 9 - 11, dadurch gekennzeichnet, daß die Ankerwicklung (12) in Dreieck geschaltet ist und die Trennmittel mit jeder Wicklungsphase (13) in Reihe geschaltet sind.13. DC drive according to one of claims 9 - 11, characterized in that the armature winding (12) in Triangle is connected and the separating means are connected in series with each winding phase (13).
14. Gleichstromantrieb nach einem der Ansprüche 2 - 13, dadurch gekennzeichnet, daß die Schaltvorrichtung (11) Halbleiterschalter (15) in Brückenschaltung aufweist, daß die den Fehlerfall erkennende Steuereinheit (17) in jeder Verbindungsleitung (14) zwischen Schaltervorrichtung (11) und Ankerwicklung (12) angeordnete Meßshunts (18) aufweist und daß die14. DC drive according to one of claims 2-13, characterized in that the switching device (11) has semiconductor switches (15) in a bridge circuit, that the fault-detecting control unit (17) in each connecting line (14) between the switch device (11) and armature winding (12) arranged measuring shunts (18) and that
Steuereinheit (17) in gleichzeitigen Sperrphasen aller Halbleiterschalter (15) die über die Meßshunts (18) fließenden Ströme mißt und bei Auftreten eines signifikant von Null abweichenden Stromwerts in mindestens einem der Meßshunts (18) einControl unit (17) measures the currents flowing over the measuring shunts (18) in the simultaneous blocking phases of all semiconductor switches (15) and in at least one of the measuring shunts (18) if a current value which differs significantly from zero occurs
Aktivierungssignal an die Trennmittel ausgibt.Outputs activation signal to the release agent.
15. Gleichstromantrieb nach einem der Ansprüche 2 - 13, dadurch gekennzeichnet, daß die den Fehlerfall erkennende Steuereinheit (17) Meßshunts (21) aufweist, die jeweils eine Wicklungsphase (13) der Ankerwicklung (12) mit dem Sternpunkt (20) verbinden, und daß die Steuereinheit (17) fortlaufend die Shuntströme nach Betrag und Phase mißt und vektoriell addiert und bei signifikantem Abweichen der Vektorsumme von Null ein Aktivierungssignal an die Trennmittel gibt. 15. DC drive according to one of claims 2-13, characterized in that the fault-detecting control unit (17) has measuring shunts (21), each connecting a winding phase (13) of the armature winding (12) to the star point (20), and that the control unit (17) continuously measures the shunt currents according to magnitude and phase and adds them vectorially and, if the vector sum deviates significantly from zero, gives an activation signal to the separating means.
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US6759823B2 (en) 2004-07-06
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US20020105239A1 (en) 2002-08-08

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